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空间用S4R电源功率调节器研究与仿真 被引量：2

The Emluator and Research of the Controller Based on the Space Power System
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摘要 对基于S4R的以太阳能电池阵-蓄电池组-功率控制器为基础的电源功率调节系统进行了分析,应用Saber仿真软件对S4R功率控制系统进行了仿真,深入研究了S4R功率控制供电/充电/分流的3种工作状态,仿真结果表明S4R功率调节器能够自主调节母线输出,具有良好的电性能。 To analyse the power system topology which is based on the solar cell panels-battery-power control system,depended on S4R（the sequential switching shunt series regulator）.The power control system of S4R power control unit is simulated by the Saber,and the S4R system was analyzed and proved the supply/charge/shunt working state.The result indicates that S4R power regulate system can self-regulate the power export,and the electricity performance is very well.
作者 铁琳 张朋松
机构地区 上海交通大学电子信息与电气工程学院 上海卫星工程研究所
出处 《机械与电子》 2010年第11期54-57,共4页 Machinery & Electronics
关键词 电源功率调节器 S4R SABER仿真 space power system S4R Saber emluator
分类号 V242.2 [航空宇航科学与技术—飞行器设计]
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参考文献5

  • 1张朋松.新型空间电源功率控制系统研究与设计[D].西安:西北工业大学.2010.
  • 2Garrigos Ausias,et al. System model of the sequential switching shunt series regulator for spacecraft regulated high power busses[A]. 35^th Annual IEEE Power Electronics Speciation Conference[C]. 2004.
  • 3雷卫军,李言俊.S4R功率调节技术在航天器上的仿真研究与实现[J].宇航学报,2008,29(3):977-982. 被引量：5
  • 4李瑜.空间一次电源功率控制系统设计[D].西安:西北工业大学,2009.
  • 5Garrigos Ausias, Carraseo Jose A, Blanes jose M, Francisco Garcia de Quiros. A Power Conditioning Unit for High Power GEO Satellites Based on the Sequential Switching Shunt Series Regulator[Z]. 1EEE.2006.

二级参考文献6

  • 1Capel A, Perol P. Comparative performance evaluation between the S4R and the S3R regulated bus topologies [ C ]. Rec. IEEE Power Electronics Specialists Conf., 2001 : 1963 - 1969.
  • 2Capel A, O'Sullivan D, Marpinard J C. High power conditioning for space applications[J]. Proc. IEEE, 1988, 76(4): 391-408.
  • 3Garrigos A, Carrasco J A. Blanes J M, Sanchis-Kilders E. A powerconditioning unit for high power GEO satellites based on the sequential switching shunt series regulator[J]. Electrotechnical Conference, MELECON 2006. IEEE Mediterranean, 2006: 1186- 1189.
  • 4Lee D H, Cho B H. Patil A R, Lee F C. Design of a single PWM section shunt switching unit for high power space system[J]. IEEE Power Electronics Specialists 1995 : 145 - 149.
  • 5Weijun lei, Yanjun Li. Modeling and analysis of 1 .5kW BPR for Power condition unit in high-power satellites. Submitted for Publication.
  • 6Garrigos A, Carrasco A. System model of the sequential switching shunt series regulator for spacecraft regulated high power busses [ J ]. Annual IEEE Power Electronics Specialists Conf., 2004:2645 - 2650.

共引文献6

同被引文献16

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机械与电子
2010年 第11期

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